Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek (from gpkit.tests.from_paths.TestFiles-20171116085017)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.03574700899e-13.
Allowing negative dual variable(s) as small as -2.01698466956e-12.
Allowing negative dual variable(s) as small as -2.16843383527e-12.
Allowing negative dual variable(s) as small as -2.15937294087e-12.
Solving took 4 GP solves and 3.52 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.01497803218e-13.
Allowing negative dual variable(s) as small as -1.98525701087e-12.
Allowing negative dual variable(s) as small as -2.17011998649e-12.
Allowing negative dual variable(s) as small as -2.16463479086e-12.
Solving took 4 GP solves and 3.09 seconds.
Allowing negative dual variable(s) as small as -1.21177373691e-13.
Allowing negative dual variable(s) as small as -8.13229691921e-14.
Allowing negative dual variable(s) as small as -2.06449440876e-14.
Allowing negative dual variable(s) as small as -2.07741809866e-14.
Allowing negative dual variable(s) as small as -1.04416540518e-12.
Allowing negative dual variable(s) as small as -1.64586530169e-12.
Allowing negative dual variable(s) as small as -1.46424994525e-12.
Allowing negative dual variable(s) as small as -1.46802535406e-12.
MTOW [lbs] = 132.53
Zero fuel weight [lbs] = 53.63
Wing span [ft] = 24.00
Aicraft length [ft] = 12.90
Aspect ratio = 25.60
mean aerodynamic chord [ft] = 0.9722
root chord [ft] = 1.250
speed for best rate of climb [m/s]: Vy = 20.352
speed at top of climb [m/s] = 25.000
design loiter speed [m/s] = 25.000
rotation speed at 55 lbs [m/s] = 18.158
rotation speed at 150 lbs [m/s] = 27.301
Allowing negative dual variable(s) as small as -1.12473528754e-12.
Allowing negative dual variable(s) as small as -1.65571722999e-12.
Allowing negative dual variable(s) as small as -1.63824119201e-12.
Allowing negative dual variable(s) as small as -1.63490315036e-12.
optimum loiter speed for min power, start of loiter [m/s] = 23.618
optimum loiter speed for min power, end of loiter [m/s] = 16.685
optimum cruise speed, inbound [m/s] = 31.024
optimum cruise speed, outbound [m/s] = 23.411
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.25445110107e-11.
Allowing negative dual variable(s) as small as -4.86406946986e-11.
Allowing negative dual variable(s) as small as -4.1382023172e-12.
Allowing negative dual variable(s) as small as -4.13940686501e-12.
Solving took 4 GP solves and 3.37 seconds.
Max Speed [m/s]: 64.61
Beginning signomial solve.
Solving took 4 GP solves and 1.95 seconds.
Max payload weight [lbf] = 8.892
Max take off weight [lbf] = 140.364
Allowing negative dual variable(s) as small as -1.21123597263e-13.
Allowing negative dual variable(s) as small as -8.15172582214e-14.
Allowing negative dual variable(s) as small as -2.06779038336e-14.
Allowing negative dual variable(s) as small as -2.06553524285e-14.
Allowing negative dual variable(s) as small as -1.04304022017e-12.
Allowing negative dual variable(s) as small as -1.65013207092e-12.
Allowing negative dual variable(s) as small as -1.4655705035e-12.
Allowing negative dual variable(s) as small as -1.46658770198e-12.
MTOW [lbs] = 132.53
Zero fuel weight [lbs] = 53.63
Wing span [ft] = 24.00
Aicraft length [ft] = 12.90
Aspect ratio = 25.60
mean aerodynamic chord [ft] = 0.9722
root chord [ft] = 1.250
speed for best rate of climb [m/s]: Vy = 20.352
speed at top of climb [m/s] = 25.000
design loiter speed [m/s] = 25.000
rotation speed at 55 lbs [m/s] = 18.158
rotation speed at 150 lbs [m/s] = 27.301
Allowing negative dual variable(s) as small as -1.12398935645e-12.
Allowing negative dual variable(s) as small as -1.65818292257e-12.
Allowing negative dual variable(s) as small as -1.64072618339e-12.
Allowing negative dual variable(s) as small as -1.63356741328e-12.
optimum loiter speed for min power, start of loiter [m/s] = 23.618
optimum loiter speed for min power, end of loiter [m/s] = 16.685
optimum cruise speed, inbound [m/s] = 31.024
optimum cruise speed, outbound [m/s] = 23.411
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.25444839633e-11.
Allowing negative dual variable(s) as small as -4.86404095245e-11.
Allowing negative dual variable(s) as small as -4.13816654488e-12.
Allowing negative dual variable(s) as small as -4.13948438999e-12.
Solving took 4 GP solves and 3.11 seconds.
Max Speed [m/s]: 64.61
Beginning signomial solve.
Solving took 4 GP solves and 2.09 seconds.
Max payload weight [lbf] = 8.892
Max take off weight [lbf] = 140.364
	

Standard Error